An experimental study on gust load alleviation using passive ventilation wing concept

Yasuhiro Tani, Shuhei Seki, Shigeru Aso

研究成果: Chapter in Book/Report/Conference proceedingConference contribution

5 被引用数 (Scopus)

抄録

To reduce the gust load on aircraft wings, a new gust load alleviation method using passive ventilation concept with porous surface and deflectable vanes has been proposed. To confirm the effect of this concept, low speed wind tunnel test was conducted on the wing models with two types of gust load alleviation mechanisms. To measure the gust response aerodynamic forces, a gust generator was installed to a low speed wind tunnel in Kyushu University. Three component aerodynamic forces were measured for the steady flow and unsteady gust flow conditions, and it was confirmed that the proposed concept provides the reduction of gust load for aircraft wings with simple mechanisms.

本文言語英語
ホスト出版物のタイトルAIAA Aerospace Sciences Meeting
出版社American Institute of Aeronautics and Astronautics Inc, AIAA
210059
ISBN(印刷版)9781624105241
DOI
出版ステータス出版済み - 1 1 2018
イベントAIAA Aerospace Sciences Meeting, 2018 - Kissimmee, 米国
継続期間: 1 8 20181 12 2018

出版物シリーズ

名前AIAA Aerospace Sciences Meeting, 2018
番号210059

その他

その他AIAA Aerospace Sciences Meeting, 2018
Country米国
CityKissimmee
Period1/8/181/12/18

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering

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